Solar Tracker

ABSTRACT

A solar tracker comprises a support frame, a panel assembly comprising one or more solar panels, and an actuator to rotate the panel assembly to track the movement of the sun. The panel assembly comprises a central spine and one or more panel carriers extending transversely over the top of the central spine for supporting solar panels. The panel carriers are secured to the central spine by respective support brackets. The support brackets comprise a top surface, side walls extending downwardly from opposing sides of the top surface, and a slot with a downwardly facing opening extending transversely through the sidewalls. The slot is configured to receive the central spine.

CROSS-REFERENCE TO RELATED APPLICATIONS

The present application is a continuation of U.S. patent application Ser. No. 15/784,816, filed on Oct. 16, 2017, which is a continuation of U.S. patent application Ser. No. 14/700,413, filed on Apr. 30, 2015, U.S. Pat. No. 9,793,851, which is a Continuation in Part which claimed priority to U.S. patent application Ser. No. 12/830,907, filed on Jul. 6, 2010, U.S. Pat. No. 9,057,546, the disclosures of all of which are incorporated by reference herein in their entirety.

BACKGROUND

The present invention relates generally to solar panels for generating solar energy and, more particularly, to a free-standing solar tracker with a rotating panel assembly to track the movement of the sun during the day.

Photovoltaic panels, or solar panels, have been used for a long time in commercial and residential applications. A solar panel typically comprises a plurality of photovoltaic cells, also known as solar cells, that convert sunlight into electricity. In most commercial or residential applications, a large array of solar panels is needed to generate enough energy to have any practical effect. Thus, the use of solar panels requires a relatively large amount of open space exposed to direct sunlight. Most often, solar panels are mounted on the roofs of homes and buildings. In most installations, the solar panels are mounted in a fixed position to maximize the exposure when the sun is at its peak.

Conventional solar systems have not gained widespread acceptance for a number of reasons, including the cost of the solar systems, the availability of adequate space, and aesthetic reasons. Conventional solar systems typically cost more than other available energy sources. The added expense of solar systems is an impediment to adoption of solar systems. Also, many people who are willing to pay the extra cost of a solar system may not be able to do so because they lack adequate space exposed to the sun. Others may consider solar panels mounted on the roofs of homes to be aesthetically unappealing. Concerns over the aesthetics of the solar panels are another impediment to adoption of solar systems.

Therefore, there is a continuing need for a solar system that is relatively inexpensive, that can be deployed in a relatively small area, and overcome concerns regarding aesthetics of the solar panels.

SUMMARY

The present invention provides a solar tracker that can be used for both residential and commercial applications. The solar tracker comprises a support frame, a panel assembly including one or more solar panels, and an actuator to rotate the solar panel to track the movement of the sun. The panel assembly includes a central spine and one or more panel carriers extending transversely over the top of the central spine for supporting the solar panels. The panel carriers are secured to the central spine by respective support brackets. In some embodiments, the support brackets comprise a top surface, side walls extending downwardly from opposing sides of the top surface, and a slot with a downwardly facing opening extending transversely through the sidewalls. The slot is configured to receive the central spine.

In some embodiments, the solar tracker further comprises a base and the support frame mounts to the base to provide a free-standing solar tracker. Thus, the solar tracker can be easily moved to a site with adequate exposure to the sun. In one embodiment, the base forms an open pan to contain a ballast material for holding the solar tracker in place. In another embodiment, the base includes one or more base beams that that rest on an underlying support surface. The base is held in place by ballast containers that are filled with a ballast material and that are configured to straddle at least one of the base beams.

The solar tracker is designed to be relatively inexpensive to build and operate. Additionally, the ability to track the movement of the sun significantly increases the output of the solar panel assembly, thus increasing the user's return on the investment in the solar system. Embodiments with the free-standing support allows the solar tracker to be deployed in any location with adequate exposure. Also, the ability to deploy the solar tracker in any desired location means that the solar tracker can be deployed in locations that will not detract from the appearance of the owner's home or building.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is perspective views of a solar tracker according to a first exemplary embodiment of the invention with its solar panel in a first rotational position.

FIG. 2 is perspective views of a solar tracker according to the first exemplary embodiment of the invention with its solar panel in a second rotational position.

FIG. 3 is a front elevation of the solar tracker.

FIG. 4 is a side elevation of the solar tracker.

FIGS. 5 and 6 illustrate the mounting of the panel assembly to the support frame.

FIG. 7 illustrates the actuator assembly and mounting of the panel assembly to the support frame.

FIG. 8 illustrates the base of the solar tracker with disassembled components of a support frame and panel assembly stored inside the base.

FIG. 9 illustrates the base of the solar tracker closed to contain the disassembled components of a support frame and panel assembly.

FIG. 10 illustrates a second embodiment of the solar tracker.

FIG. 11 illustrates a third embodiment of the solar tracker.

FIG. 12 illustrates a panel assembly for the solar tracker.

FIG. 13 illustrates a support bracket in the panel assembly.

FIG. 14 illustrates the support bracket and central spine of the panel assembly.

FIG. 15 illustrates how to fabricate a plurality of support brackets from a single piece of tubular metal stock.

DETAILED DESCRIPTION

Referring now to the drawings, a solar tracker 10 according to the present invention is shown. The solar tracker 10 generally comprises a base 20, support frame 40, panel assembly 60, and actuator assembly 90 for rotating the panel assembly 60 to follow the azimuth of the sun as it moves across the sky. The solar tracker 10 is designed to be free-standing and requires no foundation. Thus, the solar tracker 10 can be easily moved between sites. The base 20 of the solar tracker is designed to serve as a “suitcase” to contain most of the components of the solar tracker 10, making it easier to transport the solar tracker 10 to a location where the solar tracker is installed.

The base 12 of the solar tracker 10 is formed in two sections 22 that are connected to one another by a hinge 24. The base sections 22 are movable between an open or deployed position (FIG. 8) and a closed or storage position (FIG. 9). Each section 22 comprises a pair of side members 26 and a pair of end members 28 forming a generally-rectangular frame. The side members and end members may be constructed of a metal tubing, metal channel, or metal beam. A bottom sheet 30 made of a sheet metal is fixedly attached to the frame such as by welding to form an open pan in the deployed position. Separators 32 are spaced longitudinally between the end members 28 and extend between the side members 26. The separators 32 may be inserted into tracks or channels (not shown) in the side members 26 so that the separators can be removed. In a preferred embodiment, the separators 32 are formed of a sheet metal and extend approximately two-thirds the height of the side members 26. The separators 32 prevent the ballast material from shifting and help maintain the ballast material evenly distributed over the pan formed by the base 20. In use, the base sections 22 are unfolded so that they lie side-by-side. The base sections 22 can then be bolted together in the open position or may be held together by the hinge 24.

The support frame 40 mounts to the base 20. The support frame 40 comprises front frame 42 and a rear frame 52. The front frame 42 comprises a pair of legs 44, a gusset plate 46, and a strut 50, which may be made of metal and removably connected together by bolts and nuts, or other suitable fasteners. The legs 44 may be made of rigid material, such as a metal angle. The legs 44 extend upwardly at an angle from the one end of the base 20. The lower ends of the legs 44 are bolted or otherwise secured to respective end members 28 of the base 20. The upper end of the legs 44 are connected by a gusset plate 46, which may be made of a metal plate. The gusset plate 46 provides rigidity to the frame 42, as well as provides a surface for mounting the panel assembly 60 as hereinafter described. Strut 50 is made of a rigid material, such as a metal angle, and provides lateral stability for the front frame 42. The strut 50 is connected at the lower end to the side members 26 of the base 20, and at the upper end to the gusset plate 46 of the frame 42.

The rear frame 50 includes a pair of legs 52, gusset plate 52, and strut 56, which may be made of metal and removably connected together by bolts and nuts, or other suitable fasteners. The legs 52 extend upwardly at an angle from respective end members 28 of the base 20. The lower ends of the legs 52 are bolted or otherwise secured to the end members 28, while the upper ends of the legs 52 are connected by the gusset plate 54, which may be made of a metal plate. Strut 56 extends between the base 20 and gusset plate 54 to provide lateral stability to the rear frame 52. It may be noted that the rear frame 50 is tilted at a slight angle relative to the base 20, whereas the front frame 42 is perpendicular to the base 20. The exact orientation of the frames 42, 50, however, is not material. Depending on the size of the frame 42, reinforcing members 58 may be provided to interconnect the legs 52 at spaced locations.

The panel assembly 60 comprises a plurality of solar panels 62 and a panel support frame 64 to support the solar panels. The panel support frame 64 comprises a central spine 66, a pair of laterally-spaced side members 68, and a plurality of longitudinally-spaced panel carriers 70, which can be removably connected by bolts and nuts, or other fasteners. The panel carriers 70 include an inner end and an outer end. The inner end connects to the spine 66 and while the side member 78 connect to the outer ends of the panel carriers 70. The spine 66 in the exemplary embodiment is made from a metal tube, while the side members 68 and panel carriers are made of a metal channel. The panel carriers 70 taper from the inner end to the outer end. The side members 68 are spaced from the spine 66 so that the inner ends of the solar panels rest on a top surface of the spine 66, while the outer ends of the solar panels rest on a top surface of the side members 68. The panel carriers 70 are longitudinally-spaced so that the side edges of the solar panels 62 rest on the top surfaces of respective wing member 70. The solar panel 62 can be removably secured to the panel support frame 64 by bolts, screws, clamps, or other mechanical fastening devices.

The panel assembly 60 is rotatably mounted to the support frame 40 so as to rotate about a single, inclined axis. FIG. 5 shows a first mounting assembly 80 for securing the lower end of the panel assembly 60 to the front support frame 42. The first mounting assembly 80 comprises a connecting plate 82, L-shaped mounting brackets 84, bearing 86, and a pivot member 88. The connecting plate 82 is bolted, welded, or otherwise secured to the gusset plate 46 of the front frame 42. The connecting plate 82 is bent at a slight angle to provide the desired tilt for the rotational axis of the panel assembly 60. Mounting brackets 84 are bolted or welded to the spine 66 of the panel support frame 64. The upper end of connecting plate 82 and bearing 66 are disposed between the brackets 86. Pivot member 88, such as a bolt, passes through the mounting brackets 84, connecting plate 82, and bearing 86, and is secured by a conventional nut threaded onto the end of the pivot member 88.

FIGS. 6 and 7 shows a second mounting assembly 90 for mounting the upper end of the panel support frame 64 to the rear support frame 50. The second mounting assembly 90 comprises a connecting plate 92, a pair of mounting forks 94, a bearing 96, and a pivot member 98. Connecting plate 92 is secured by bolts or other mechanical fasteners to the gusset plate 56 of the rear support frame 50. The mounting forks 94 include a slot 95 to receive the spine 66 of the panel support frame 64. The mounting forks 94 may be permanently fixed to the spine 66 by welding. Bearing 96 is disposed between the lower end of the mounting forks 94. Pivot member 98 extends through the mounting forks 94, upper end of connecting plate 92, and bearing 96, and is secured in place by a nut threaded onto the end of the pivot member 98.

Pivot member 88 on the first mounting assembly 80 and pivot member 98 on the second mounting assembly 90 are co-axially aligned along the axis and rotation of the panel assembly 60. The rotational axis inclines upwardly from front to rear in a plane perpendicular to the base 20. The rotational axis is aligned when deployed so that the plane of the rotational axis aligns with the sun at the highest altitude. Thus, the panel assembly 60 can rotate to track the path of the sun as the sun travels across the sky during the day.

Actuator assembly 100, shown in FIG. 7, comprises a pivot arm 102, fluid cylinder 102, and control unit 106. Pivot arm 102 is connected at one end to the spine 66 of the panel support frame 64. Pivot arm 102 extends outward from the spine 66. Fluid cylinder 104 is connected at one end to the pivot arm 102 and the opposite end to the front Frame. Control unit 106 is mounted to the front Frame and controls operation of the fluid cylinder 104. The extension of the fluid cylinder 104 rotates the panel assembly 60 in a first direction, while retraction of the fluid cylinder 104 rotates the panel assembly 60 in the opposite direction. The control unit 106 preferably includes a processor and associated memory for controlling the rotation of the panel assembly 60. The control unit 106 may store ephemeras data in memory that gives the position of the sun in the sky at different times of the day. Alternatively, the position of the sun in the sky at different times of day may be calculated based on formulas that model the sun's movement. As the azimuth of the sun changes, the control unit 106 rotates the panel assembly 60 to minimize as much as possible the angle of incidence of the sun rays on the solar panels 62. It is noted that the panel assembly 60 rotates about a single axis that follows the azimuth of the sun. Those skilled in the art will appreciate that it is also possible to change the angle of inclination of the solar panels to track changes in the altitude of the sun.

As previously noted, the solar tracker 10 is designed so that most of the components can be disassembled and packaged in the base 20. FIG. 8 shows the base 20 with the base sections 22 folded open. FIG. 9 shows the panel carriers 70 stored in one of the base sections 22. Components of the support frame 40 may, likewise, be disposed in one of the base sections. Essentially all of the components, with the exception of the spine 66 and solar panels 62, will fit inside the base sections 22. The base sections 22 can then be folded to a closed position as shown in FIG. 9 to form a suitcase with a compartment containing most of the solar tracker components.

FIG. 10 shows an alternate embodiment of the solar tracker. This embodiment is the same as the first embodiment except for the construction of the bas, which is designated by reference number 120 in this embodiment. The base 120 comprises an I-shaped frame having center beam 122 and a pair of end beam 124. The end beams 124 may be secured to the center beam 122 by bolting, welding, or other suitable means.

The base 120 is designed to lie on a flat surface. The base 120 is held in place by specially-designed ballast containers 130 that contain a ballast material, such as sand, gravel, water, etc. In the exemplary embodiment shown in FIG. 6, the ballast containers 130 comprise open containers having a bottom 132, side walls 134, and open top 136. A channel 138 is formed in the bottom 132 of the ballast containers 130 so that the center beam 122 of the base 120 can pass through the ballast containers 130 as shown in FIG. 10. Thus, the ballast containers 130 effectively straddle the center beam 122 of the base 120. Once the ballast containers 130 are placed on the center beam 122 as shown in FIG. 100, the ballast containers 130can be filled with a ballast material (e.g., gravel, sand, water, etc) to hold the base 120 in place.

While the embodiment shown in FIG. 6 contains the ballast material in open ballast containers 130, those skilled in the art will appreciate that closed ballast containers 130 could also be used. For example, the ballast container 130 may comprise a closed container with a fill hole for filling the ballast container 130 with water or other fluid. The ballast container 130 could be formed with handle or other features for carrying the ballast containers 130. The ballast containers 130 may also have features for stacking and/or nesting the ballast containers 130.

FIG. 11 shows a third embodiment of the solar tracker. Like, the previous embodiment the base 120 comprises an I-shaped frame having center beam 122 and a pair of end beams 124. The end beams 124 may be secured to the center beam 122 by bolting, welding, or other suitable means. In the illustrated embodiment, the center beam 122 and end beams are metal tubes. Those skilled in the art will appreciate that the center beam 122 and end beams 124 may also comprise metal channels, metal I-beams, or other structural members.

The base 120 is designed to lie on a flat surface. The base 120 is held in place by anchor members 140 that are embedded in the ground or other support surface. Anchor brackets 142 connect the anchor members to the end beams 124 of the base 120.

The present invention provides a free-standing solar tracker 10 that can be easily transported to a desired location and installed. The solar tracker assembly 10 is designed to be free-standing and does not require any foundation. The solar tracker 10 rests on the surface of the ground and is held in place by ballast material. If desired, the solar tracker assembly 10 may be placed on a concrete pad, but there is no need in most instances to fasten the solar tracker to the concrete pad. However, those skilled in the art will appreciate that tie-down straps or other securing devices could be used in conjunction with the ballast material, particularly where very high winds are expected. The base of the solar tracker assembly is designed to serve as a “suitcase” for transporting the components of the solar tracker 10. As noted previously, most of the components of the solar tracker, with the exception of the spine 66 and solar panels 72, can be packaged within the base 20 for transportation and storage.

FIGS. 12-14 illustrate an alternate embodiment of the panel assembly 60. For convenience, similar reference numbers are used herein to indicate similar parts. The panel assembly 60 includes a plurality of panels 62 and a panel support frame 64. The panel support frame 64 includes a central spine 66 and a plurality of longitudinally spaced panel carriers 70. The central spine 66 is made from a metal tube. The panel carriers 70 are made from metal channels. The panel carriers 70 are mounted on top of the central spine 66 by support brackets 50. The support bracket 150 is welded to the central spine 66.

FIGS. 13 and 14 illustrate the support bracket 150 in more detail. The support bracket 150 comprises a top surface 152, opposing sidewalls 154, and crossbars 156 that connect the lower edge of the sidewalls 154. A slot 158 extends transversely through the sidewalls 154. The slot 158 is open at its lower end and configured to receive the central spine 66, as shown in FIG. 14. The support bracket 150 may be secured to the central spine 66 by welding. The top surface 152 of the support bracket 150 may include bolt holes 160 to receive bolts that secure the panel carrier 70 to the support bracket 150. Once the panel carrier 70 is bolted to the support bracket 150, the panel carrier 70 can be further secured by spot welding the panel carrier 70 to the support bracket 150.

FIG. 15 illustrates a method of fabricating the support brackets 150 from tubular metal stock. FIG. 15 shows 6 support brackets labeled 150A through 150F fabricated from a single piece of tubular stock. A laser tube-cutting machine, such as the LT8 laser tube cutter by BLM Group, may be used to cut the metal tube. The support brackets 150 are designed so that the sidewalls 154 of the support brackets 150 overlap. Adjacent support brackets 150 are inverted. Thus, as seen in FIG. 15, support brackets 150A, 150C and 150E are oriented with the open end of the slot 158 facing down. Support brackets 150B, 150D and 150F are oriented with the slots 158 facing up. The support brackets 150 are formed by cutting the slots 158 and cutting diagonally through the metal between adjacent support brackets 150.

The present invention may, of course, be carried out in other specific ways than those herein set forth without departing from the scope and essential characteristics of the invention. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, and all changes coming within the meaning and equivalency range of the appended claims are intended to be embraced therein. 

What is claimed is:
 1. A frame assembly for a solar tracker comprising: a support frame; a panel assembly rotatably mounted to said support frame configured to support one or more solar panels, said panel assembly including: a central spine rotatably mounted to the support frame; and a plurality of panel carriers extending transversely over the top of the central spine and extending outwardly from opposing sides of the central spine; and one or more supports for securing respective panel carriers to the central spine; a mounting assembly for rotatably mounting the panel assembly to the support frame, said mounting assembly comprising: a mounting member configured to be rotatably connected to said support frame; and an open-ended slot in said mounting member configured to receive the central spine of the panel assembly; and an actuator assembly for rotating the panel assembly to track the movement of the sun; and 